This document is the result of a collaborative effort between NASA's Johnson Space Center, Marshall Space Flight Center, Glenn Research Center, and the United States Air Force Research Laboratory at Wright Patterson AFB in support of the Space Shuttle Orbiter Upgrades Program, specifically the Electric Auxiliary Power Unit Program. This document is intended as a guideline for design applications for corona and partial discharge avoidance and is not a requirements specification instrument.Hall, David K. and Kirkici, Hulya and Schweickart, Dan L. and Dunbar, William and Hillard, BarryGlenn Research Center; Johnson Space Center; Marshall Space Flight CenterELECTRIC CORONA; SPACE SHUTTLE ORBITERS; AUXILIARY POWER SOURCES; SPACE TRANSPORTATION SYSTEM; FUSELAGES; PLASMA DENSITY; ELECTRONIC PACKAGING; SEALING; CIRCUIT BOARDS...